A cross influence between the blade pitch angle and the servo blade flapping angle is studied. A full mechanical equations of a rigid body motion was taken as a basis for a description of the flapping motion process. It was found that the dimensionless variables in the equations can be divided into groups by their decimal orders. The equations were truncated up to the second order of approximation error.
Original languageEnglish
Title of host publicationProceedings of the 6th European Conference for Aerospace Sciences
StatePublished - 2015
Externally publishedYes

ID: 4749617